EP3413001A1 - Échangeur de chaleur fabriqué par production additive - Google Patents

Échangeur de chaleur fabriqué par production additive Download PDF

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Publication number
EP3413001A1
EP3413001A1 EP17425060.5A EP17425060A EP3413001A1 EP 3413001 A1 EP3413001 A1 EP 3413001A1 EP 17425060 A EP17425060 A EP 17425060A EP 3413001 A1 EP3413001 A1 EP 3413001A1
Authority
EP
European Patent Office
Prior art keywords
plenum
heat exchanger
cowl
heat exchange
component
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP17425060.5A
Other languages
German (de)
English (en)
Other versions
EP3413001B1 (fr
Inventor
Antonio CAIMANO
Antonio Cardillo
Ivan Fanelli
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GE Avio SRL
Original Assignee
GE Avio SRL
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by GE Avio SRL filed Critical GE Avio SRL
Priority to EP17425060.5A priority Critical patent/EP3413001B1/fr
Priority to US15/976,206 priority patent/US11236674B2/en
Priority to CA3006128A priority patent/CA3006128A1/fr
Priority to JP2018104179A priority patent/JP2019023554A/ja
Priority to CN201810573726.2A priority patent/CN108999706B/zh
Publication of EP3413001A1 publication Critical patent/EP3413001A1/fr
Application granted granted Critical
Publication of EP3413001B1 publication Critical patent/EP3413001B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/16—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
    • F28D7/1615—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation the conduits being inside a casing and extending at an angle to the longitudinal axis of the casing; the conduits crossing the conduit for the other heat exchange medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/06—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
    • F28F13/12—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media by creating turbulence, e.g. by stirring, by increasing the force of circulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/12—Elements constructed in the shape of a hollow panel, e.g. with channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F9/026—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits
    • F28F9/0265—Header boxes; End plates with static flow control means, e.g. with means for uniformly distributing heat exchange media into conduits by using guiding means or impingement means inside the header box
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/324—Application in turbines in gas turbines to drive unshrouded, low solidity propeller
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/53—Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/02—Header boxes; End plates
    • F28F2009/0285—Other particular headers or end plates
    • F28F2009/0287—Other particular headers or end plates having passages for different heat exchange media
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
EP17425060.5A 2017-06-06 2017-06-06 Échangeur de chaleur fabriqué par production additive Active EP3413001B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP17425060.5A EP3413001B1 (fr) 2017-06-06 2017-06-06 Échangeur de chaleur fabriqué par production additive
US15/976,206 US11236674B2 (en) 2017-06-06 2018-05-10 Additively manufactured heat exchanger
CA3006128A CA3006128A1 (fr) 2017-06-06 2018-05-24 Echangeur de chaleur fabrique de maniere additive
JP2018104179A JP2019023554A (ja) 2017-06-06 2018-05-31 付加製造による熱交換器
CN201810573726.2A CN108999706B (zh) 2017-06-06 2018-06-06 增材制造的热交换器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP17425060.5A EP3413001B1 (fr) 2017-06-06 2017-06-06 Échangeur de chaleur fabriqué par production additive

Publications (2)

Publication Number Publication Date
EP3413001A1 true EP3413001A1 (fr) 2018-12-12
EP3413001B1 EP3413001B1 (fr) 2020-01-08

Family

ID=59315571

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17425060.5A Active EP3413001B1 (fr) 2017-06-06 2017-06-06 Échangeur de chaleur fabriqué par production additive

Country Status (5)

Country Link
US (1) US11236674B2 (fr)
EP (1) EP3413001B1 (fr)
JP (1) JP2019023554A (fr)
CN (1) CN108999706B (fr)
CA (1) CA3006128A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3663541A1 (fr) * 2018-12-03 2020-06-10 United Technologies Corporation Système de gestion thermique pour moteur à turbine à gaz
FR3097272A1 (fr) * 2019-06-14 2020-12-18 Safran Helicopter Engines Dispositif de controle de debit de fluide

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FR3084698B1 (fr) * 2018-07-31 2020-07-24 Safran Aircraft Engines Echangeur thermique pour turbomachine
US11054197B2 (en) * 2018-12-19 2021-07-06 Unison Industries, Llc Heat exchanger and methods of forming
IT201900012924A1 (it) * 2019-07-25 2021-01-25 Ge Avio Srl Sotto-sistema di raffreddamento integrato
FR3100269B1 (fr) * 2019-08-26 2021-09-24 Airbus Systeme propulsif pour un aeronef, ledit systeme propulsif comportant un systeme d’echangeur thermique
US11543187B2 (en) 2019-09-06 2023-01-03 Hamilton Sundstrand Corporation Heat exchanger with build powder in barrier channels
US11692479B2 (en) * 2019-10-03 2023-07-04 General Electric Company Heat exchanger with active buffer layer
CA3192175A1 (fr) * 2020-09-08 2022-03-17 Pradeep Dass Turbostatoreacteur
US11965463B2 (en) * 2021-02-16 2024-04-23 Pratt & Whitney Canada Corp. Fluid cooler installation and method for turbofan engine
US11885240B2 (en) 2021-05-24 2024-01-30 General Electric Company Polska sp.z o.o Gas turbine engine with fluid circuit and ejector
US11859500B2 (en) 2021-11-05 2024-01-02 General Electric Company Gas turbine engine with a fluid conduit system and a method of operating the same
US11788425B2 (en) 2021-11-05 2023-10-17 General Electric Company Gas turbine engine with clearance control system
US11719115B2 (en) 2021-11-05 2023-08-08 General Electric Company Clearance control structure for a gas turbine engine
FR3132082A1 (fr) * 2022-01-26 2023-07-28 Airbus Operations Ensemble pour aéronef comportant un mât et un échangeur thermique fixé sur le mât par l’intermédiaire d’un module support
US20230374938A1 (en) * 2022-05-19 2023-11-23 Raytheon Technologies Corporation Hydrogen fueled turbine engine condenser duct

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EP3012436A1 (fr) * 2014-10-21 2016-04-27 United Technologies Corporation Système d'échangeur de chaleur canalisé fabriqué de manière additive

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US20050268612A1 (en) * 2004-04-24 2005-12-08 Rolls-Royce Plc Engine
US20080230651A1 (en) * 2005-09-26 2008-09-25 Airbus France Turbofan Provided With a Pre-Cooler
EP2620618A2 (fr) * 2012-01-25 2013-07-31 Honeywell International Inc. Système d'air de refroidissement embarqué refroidi de moteur à turbine à gaz
WO2015092251A1 (fr) * 2013-12-19 2015-06-25 Snecma Turbomachine d'aéronef comportant un échangeur de chaleur du type pré-refroidisseur
EP3012436A1 (fr) * 2014-10-21 2016-04-27 United Technologies Corporation Système d'échangeur de chaleur canalisé fabriqué de manière additive

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3663541A1 (fr) * 2018-12-03 2020-06-10 United Technologies Corporation Système de gestion thermique pour moteur à turbine à gaz
US11519295B2 (en) 2018-12-03 2022-12-06 Raytheon Technologies Corporation Thermal management system for gas turbine engine
US11958623B2 (en) 2018-12-03 2024-04-16 Rtx Corporation Thermal management system for gas turbine engine
FR3097272A1 (fr) * 2019-06-14 2020-12-18 Safran Helicopter Engines Dispositif de controle de debit de fluide

Also Published As

Publication number Publication date
US20180347468A1 (en) 2018-12-06
CN108999706A (zh) 2018-12-14
EP3413001B1 (fr) 2020-01-08
US11236674B2 (en) 2022-02-01
CA3006128A1 (fr) 2018-12-06
CN108999706B (zh) 2021-06-04
JP2019023554A (ja) 2019-02-14

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